Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing

ZHEN Wen-qiang;JI Yong-qiang;SHI Yun-guo

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  • Sponsored by: China Association for Science and Technology (CAST)

    Editor-In-Chief: Xu Yida

    ISSN 1000-1093

    　

  • Hosted By: China Ordnance Society

    Published By: Acta Armamentarii

    CN 11-2176/TJ

Acta Armamentarii, a Chinese monthly journal, was first published in 1979. The journal is supervised by China Association for Science and Technology, sponsored by China Ordnance Society，and edited and published by Editorial Board of Acta Armamentarii. The Journal is included in all important domestic databases，and also collected by Engineering Index (EI, USA), Chemical Abstracts (CA, USA), Science Abstracts (SA, UK）, Abstract Journal (AJ, Russia), and Current Bibliography on Science and Technology(CBST).Acta Armamentarii has been selected into the journal Of Ordnance Science and Technology (Weapons Industry) Field Of High Quality Scientific and Technological Periodical Classification Catalogue (2022 edition), ranking T1, and the journal of Automotive Engineering Field of High Quality Scientific and technological Periodical classification Catalogue, ranking T2.
Acta Armamentarii ›› 2016, Vol. 37 ›› Issue (8) : 1409-1414. DOI: 10.3969/j.issn.1000-1093.2016.08.010
Paper

Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing

  • ZHEN Wen-qiang, JI Yong-qiang, SHI Yun-guo
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Abstract

The deployment process of transverse folding-wings of missiles is studied. The mathematical model and dynamic simulation model of deployment process of folding-wing in missile launching and ground tests are both established, in which the influences of friction and aerodynamic force are considered. The folding-wing were designed and manufactured. The images of deployment process of folding-wings are obtained using the high speed photography during ground test. The research results show that the test results are in good agreement with those of mathematic and dynamic simulation models. A value range of friction moment is also provided from the test results, which can support the design and application of folding-wing.

Key words

ordnance science and technology / folding-wing / deployment / dynamic simulation / experiment

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ZHEN Wen-qiang, JI Yong-qiang, SHI Yun-guo. Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing. Acta Armamentarii. 2016, 37(8): 1409-1414 https://doi.org/10.3969/j.issn.1000-1093.2016.08.010

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